Daher TBM 900 - Weight and Balance Form and Diagram (In, Lbs)

Pilot's Operating Handbook
Section 6
Weight and balance
Edition 0 - October 31, 2013
Rev. 4
Page 6.4.9
Weight and balance form and diagram (in, lbs)
Moment = Weight x Arm
CG (MAC %) =
(
Arm (in) − 172.93
)
59.45
× 100
Item
Weight
(lbs)
Arm
(in)
Moment
(in.lbs)
CG
(MAC %)
Empty weight (lbs)
Baggage
FWD
(< 110 lbs) 128.0
Front seats (lbs) 178.5
Inter. seats
- 37.5 lbs
per seat
removed
224.8
Pax
Rear
bench/net
- 52.9 lbs
per seat
removed
267.1
Pax
Cargo
(< 176 lbs)
Baggage AFT (< 220 lbs) 303.0
Zero fuel
weight
(< 6032 lbs)
Fuel (lbs) 189.8
Ramp weight (< 7430 lbs)
Taxi fuel (lbs) 189.8
Takeoff
weight
(< 7394 lbs)
Trip fuel (lbs) 189.8
Landing
weight
(< 7024 lbs)
PIM - DO NOT USE FOR FLIGHT OPERATIONS